AU593309B2 - Film cooling slot with metered flow - Google Patents

Film cooling slot with metered flow Download PDF

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Publication number
AU593309B2
AU593309B2 AU66680/86A AU6668086A AU593309B2 AU 593309 B2 AU593309 B2 AU 593309B2 AU 66680/86 A AU66680/86 A AU 66680/86A AU 6668086 A AU6668086 A AU 6668086A AU 593309 B2 AU593309 B2 AU 593309B2
Authority
AU
Australia
Prior art keywords
slot
cooled wall
outlet
wall according
metering
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
AU66680/86A
Other languages
English (en)
Other versions
AU6668086A (en
Inventor
Robert Eugene Field
James Stewart Phillips
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
RTX Corp
Original Assignee
United Technologies Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of AU6668086A publication Critical patent/AU6668086A/en
Application granted granted Critical
Publication of AU593309B2 publication Critical patent/AU593309B2/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/186—Film cooling
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/80—Platforms for stationary or moving blades
    • F05D2240/81—Cooled platforms
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
AU66680/86A 1985-12-23 1986-12-16 Film cooling slot with metered flow Ceased AU593309B2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US06/812,100 US4726735A (en) 1985-12-23 1985-12-23 Film cooling slot with metered flow
US812100 1985-12-23

Publications (2)

Publication Number Publication Date
AU6668086A AU6668086A (en) 1987-06-25
AU593309B2 true AU593309B2 (en) 1990-02-08

Family

ID=25208502

Family Applications (1)

Application Number Title Priority Date Filing Date
AU66680/86A Ceased AU593309B2 (en) 1985-12-23 1986-12-16 Film cooling slot with metered flow

Country Status (8)

Country Link
US (1) US4726735A (ja)
EP (1) EP0227578B1 (ja)
JP (1) JPS62165502A (ja)
CN (1) CN1008291B (ja)
AU (1) AU593309B2 (ja)
CA (1) CA1274180A (ja)
DE (2) DE227578T1 (ja)
IL (1) IL81063A (ja)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU597922B2 (en) * 1985-12-23 1990-06-14 United Technologies Corporation A hollow longitudinally extending airfoil

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US6050777A (en) * 1997-12-17 2000-04-18 United Technologies Corporation Apparatus and method for cooling an airfoil for a gas turbine engine
DE59808819D1 (de) * 1998-05-20 2003-07-31 Alstom Switzerland Ltd Gestaffelte Anordnung von Filmkühlungsbohrungen
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EP1000698B1 (de) * 1998-11-09 2003-05-21 ALSTOM (Switzerland) Ltd Gekühlte Komponenten mit konischen Kühlungskanälen
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US6280140B1 (en) 1999-11-18 2001-08-28 United Technologies Corporation Method and apparatus for cooling an airfoil
EP1167690A1 (de) * 2000-06-21 2002-01-02 Siemens Aktiengesellschaft Kühlung der Abströmkante einer Gasturbinenschaufel
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US7563073B1 (en) * 2006-10-10 2009-07-21 Florida Turbine Technologies, Inc. Turbine blade with film cooling slot
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US7766618B1 (en) * 2007-06-21 2010-08-03 Florida Turbine Technologies, Inc. Turbine vane endwall with cascading film cooling diffusion slots
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US20100008759A1 (en) * 2008-07-10 2010-01-14 General Electric Company Methods and apparatuses for providing film cooling to turbine components
US8057182B2 (en) * 2008-11-21 2011-11-15 General Electric Company Metered cooling slots for turbine blades
US8113784B2 (en) * 2009-03-20 2012-02-14 Hamilton Sundstrand Corporation Coolable airfoil attachment section
US8672613B2 (en) 2010-08-31 2014-03-18 General Electric Company Components with conformal curved film holes and methods of manufacture
US8573938B1 (en) * 2010-11-22 2013-11-05 Florida Turbine Technologies, Inc. Turbine vane with endwall film cooling
US8893507B2 (en) 2011-11-04 2014-11-25 General Electric Company Method for controlling gas turbine rotor temperature during periods of extended downtime
GB201205020D0 (en) * 2012-03-22 2012-05-09 Rolls Royce Plc A method of manufacturing a thermal barrier coated article
WO2013188645A2 (en) 2012-06-13 2013-12-19 General Electric Company Gas turbine engine wall
US9790801B2 (en) 2012-12-27 2017-10-17 United Technologies Corporation Gas turbine engine component having suction side cutback opening
US10309239B2 (en) * 2013-02-15 2019-06-04 United Technologies Corporation Cooling hole for a gas turbine engine component
US9593590B2 (en) * 2013-03-01 2017-03-14 Siemens Energy, Inc. Active bypass flow control for a seal in a gas turbine engine
WO2014197061A2 (en) * 2013-03-15 2014-12-11 United Technologies Corporation Gas turbine engine shaped film cooling hole
WO2015047516A1 (en) * 2013-07-03 2015-04-02 General Electric Company Trench cooling of airfoil structures
US9528380B2 (en) * 2013-12-18 2016-12-27 General Electric Company Turbine bucket and method for cooling a turbine bucket of a gas turbine engine
US9957814B2 (en) 2014-09-04 2018-05-01 United Technologies Corporation Gas turbine engine component with film cooling hole with accumulator
US20160090843A1 (en) * 2014-09-30 2016-03-31 General Electric Company Turbine components with stepped apertures
US10247011B2 (en) * 2014-12-15 2019-04-02 United Technologies Corporation Gas turbine engine component with increased cooling capacity
EP3124746B1 (en) 2015-07-29 2018-12-26 Ansaldo Energia IP UK Limited Method for cooling a turbo-engine component and turbo-engine component
EP3124745B1 (en) 2015-07-29 2018-03-28 Ansaldo Energia IP UK Limited Turbo-engine component with film cooled wall
DE102016204824A1 (de) 2016-03-23 2017-09-28 Siemens Aktiengesellschaft Filmkühllöcher in Gasturbinen - Bauteilen
US10605091B2 (en) * 2016-06-28 2020-03-31 General Electric Company Airfoil with cast features and method of manufacture
US11401818B2 (en) 2018-08-06 2022-08-02 General Electric Company Turbomachine cooling trench
US11174736B2 (en) 2018-12-18 2021-11-16 General Electric Company Method of forming an additively manufactured component
US11499433B2 (en) 2018-12-18 2022-11-15 General Electric Company Turbine engine component and method of cooling
US10767492B2 (en) 2018-12-18 2020-09-08 General Electric Company Turbine engine airfoil
US11352889B2 (en) 2018-12-18 2022-06-07 General Electric Company Airfoil tip rail and method of cooling
US11566527B2 (en) 2018-12-18 2023-01-31 General Electric Company Turbine engine airfoil and method of cooling
US10844728B2 (en) 2019-04-17 2020-11-24 General Electric Company Turbine engine airfoil with a trailing edge
US11339667B2 (en) 2020-08-11 2022-05-24 Raytheon Technologies Corporation Cooling arrangement including overlapping diffusers
US11560803B1 (en) * 2021-11-05 2023-01-24 General Electric Company Component with cooling passage for a turbine engine

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US4270883A (en) * 1977-04-20 1981-06-02 The Garrett Corporation Laminated airfoil
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU597922B2 (en) * 1985-12-23 1990-06-14 United Technologies Corporation A hollow longitudinally extending airfoil

Also Published As

Publication number Publication date
IL81063A0 (en) 1987-03-31
EP0227578A2 (en) 1987-07-01
EP0227578A3 (en) 1989-04-12
DE3683742D1 (de) 1992-03-12
JPS62165502A (ja) 1987-07-22
EP0227578B1 (en) 1992-01-29
IL81063A (en) 1991-06-10
DE227578T1 (de) 1987-12-17
CN1008291B (zh) 1990-06-06
AU6668086A (en) 1987-06-25
CA1274180A (en) 1990-09-18
CN86108718A (zh) 1987-07-08
US4726735A (en) 1988-02-23

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